GENESIS 1, 29252 (Decayed)
Orbit data source: Space-Track
GENESIS 1, 29252 was a payload satellite owned by Bigelow (US) in LEO that was launched on Wed, 12 Jul 2006 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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29252 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Bigelow
Mission
Decayed Commercial Spaceship
Bus & Motor
Unknown
Mass
1,360 kg wet, 1,360 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 2.3 m
Radar Cross Section
8.133 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 GENESIS 1
1 29252U 06029A 25183.69207012 .07669060 80586-5 17140-3 0 9995
2 29252 64.4742 276.9705 0017693 300.1504 154.0455 16.44812741 50045Epoch: 2025-07-02T16:36Z
TLE epoch observation values (Epoch: 2025-07-02T16:36:34.858Z)
Latitude
64.26951°
Longitude
-153.26975°
Altitude
173.413 km
Speed
7.803 km/s
True Right ascension
01h 07m 22s
True Declination
64° 07' 22"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:28:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.095 km
Perigee altitude
139.989 km
Semi-major axis
6,529.679 km
Eccentricity
0.00177
Inclination
64.4742°
RAAN
276.9705°
Arg. of periapsis
300.1504°
True anomaly
154.13406°
Mean anomaly
154.0455°
Eccentric anomaly
154.0898°
Mean motion
4.11344 °/min
Orbital period
87.52 mins
BSTAR
0.0001714
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Other satellites on launch #29 in the year 2006 (2006-07-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GENESIS 1 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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