CYGNUS NG-24, 68689
Orbit data source: Space-Track
CYGNUS NG-24, 68689 is a payload satellite owned by NGIS (US) in LEO that was launched on Sat, 11 Apr 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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68689 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS SSG
Mission
Operational spacecraft
Bus & Motor
EPCM, Unknown motor
Mass
8,050 kg wet, 2,474 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 CYGNUS NG-24
1 68689U 26079A 26140.52007259 .00005164 00000-0 10084-3 0 9996
2 68689 51.6328 77.0641 0007497 79.3410 280.8422 15.49283153567432Epoch: 2026-05-20T12:28Z
TLE epoch observation values (Epoch: 2026-05-20T12:28:54.271Z)
Latitude
-0.00007°
Longitude
11.65946°
Altitude
418.607 km
Speed
7.662 km/s
True Right ascension
05h 08m 15s
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
07:20:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.427 km
Perigee altitude
414.235 km
Semi-major axis
6,797.468 km
Eccentricity
0.00075
Inclination
51.6328°
RAAN
77.0641°
Arg. of periapsis
79.341°
True anomaly
280.75781°
Mean anomaly
280.8422°
Eccentric anomaly
280.80001°
Mean motion
3.87278 °/min
Orbital period
92.96 mins
BSTAR
0.00010084
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Other satellites on launch #79 in the year 2026 (2026-04-11 UTC)
No other RSOs were in this launch
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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.CYGNUS NG-24 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 | 2026-05-20 23:32:33.976Z | 265.776° W | 2026-05-20 23:34:33.976Z | 308.694° NW | 29.048° | 2026-05-20 23:37:33.976Z | 34.59° NE |
| 4 mins | 2026-05-21 04:26:33.976Z | 340.108° N | 2026-05-21 04:27:33.976Z | 8.768° NNE | 28.327° | 2026-05-21 04:30:33.976Z | 93.212° ESE |
| 4 mins | 2026-05-21 06:03:33.976Z | 260.921° W | 2026-05-21 06:04:33.976Z | 232.366° WSW | 23.787° | 2026-05-21 06:07:33.976Z | 167.227° S |
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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