 Chandrayaan-2 composite |
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Mission type | Lunar orbiter, lander, rover |
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Operator | Indian Space Research Organisation (ISRO) |
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COSPAR ID | 2019-042A |
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SATCATno. | 44441 |
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Website | www.isro.gov.in/chandrayaan2-home-0 |
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Mission duration | - Orbiter: ~ 7.5 years (planned);
2 years, 10 months (elapsed)
- Vikramlander: ≤ 14 days (planned);
0 days (landing failure) - Pragyanrover: ≤ 14 days (planned);
0 days (landing failure)
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Manufacturer | Indian Space Research Organisation (ISRO) |
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Launch mass | Combined (wet): 3,850 kg (8,490 lb) Combined (dry): 1,308 kg (2,884 lb) Orbiter (wet): 2,379 kg (5,245 lb) Orbiter (dry): 682 kg (1,504 lb) Vikramlander (wet): 1,471 kg (3,243 lb) Vikramlander (dry): 626 kg (1,380 lb) Pragyanrover: 27 kg (60 lb) |
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Power | Orbiter: 1000 watts Vikramlander: 650 watts Pragyanrover: 50 watts |
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Launch date | 22 July 2019, 09:13:12 UTC |
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Rocket | GSLV Mark III M1 |
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Launch site | Satish Dhawan Space Centre Second Launch Pad |
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Contractor | Indian Space Research Organisation (ISRO) |
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Orbital insertion | 20 August 2019, 03:32 UTC |
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Pericynthion altitude | 100 km (62 mi) |
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Apocynthion altitude | 100 km (62 mi) |
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Spacecraft component | Rover |
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Landing date | 6 September 2019, 20:23 UTC |
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Landing site | Lunar south pole (intended) |
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Chandrayaan programme ← Chandrayaan-1 Chandrayaan-3 → |