SNAPPY, 69014
Orbit data source: Space-Track
SNAPPY, 69014 is an American payload satellite in SSO that was launched on Sun, 03 May 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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69014 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SNAPPY
1 69014U 26100AL 26254.68602721 .00002905 00000-0 13117-3 0 9992
2 69014 97.3941 151.1254 0007693 108.3515 251.8558 15.21739679 19961Epoch: 2026-09-11T16:27Z
TLE epoch observation values (Epoch: 2026-09-11T16:27:52.750Z)
Latitude
-0.00009°
Longitude
-86.5502°
Altitude
505.338 km
Speed
7.611 km/s
True Right ascension
10h 04m 30s
True Declination
0° 00' 00"
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
09:57:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.845 km
Perigee altitude
492.267 km
Semi-major axis
6,875.693 km
Eccentricity
0.00077
Inclination
97.3941°
RAAN
151.1254°
Arg. of periapsis
108.3515°
True anomaly
251.77205°
Mean anomaly
251.8558°
Eccentric anomaly
251.81392°
Mean motion
3.80687 °/min
Orbital period
94.57 mins
BSTAR
0.00013117
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.SNAPPY Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-12 17:50:47.940Z | 209.796° SW | 2026-09-12 17:52:47.940Z | 252.093° W | 28.523° | 2026-09-12 17:55:47.940Z | 319.982° NNW |
| 4 mins | 2026-09-13 05:20:47.940Z | 53.216° ENE | 2026-09-13 05:22:47.940Z | 96.346° ESE | 22.956° | 2026-09-13 05:24:47.940Z | 138.739° SSE |
| 4 mins | 2026-09-13 06:54:47.940Z | 324.303° NNW | 2026-09-13 06:56:47.940Z | 281.011° WNW | 20.157° | 2026-09-13 06:58:47.940Z | 245.349° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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