View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 17296U 87003B 22228.79301414 .00000249 00000-0 27223-4 0 9993
2 17296 82.5271 60.2382 0020314 118.5518 241.7745 14.83494984901691
| Epoch (UTC): | 16 August 2022 19:01:56 |
| Eccentricity: | 0.0020314 |
| inclination: | 82.5271° |
| perigee height: | 604 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 60.2382° |
| argument of perigee: | 118.5518° |
| revolutions per day: | 14.83494984 |
| mean anomaly at epoch: | 241.7745° |
| orbit number at epoch: | 90169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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