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 is defined by the following mean orbital elements,
1 00107U 26103.94370507 +.00000000 +00000-0 +11136-3 0 00003
2 00107 28.7805 326.8007 0494042 248.4325 106.2910 14.21915206 07
| Epoch (UTC): | 13 April 2026 22:38:56 |
| Eccentricity: | 0.0494042 |
| inclination: | 28.7805° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 326.8007° |
| argument of perigee: | 248.4325° |
| revolutions per day: | 14.21915206 |
| mean anomaly at epoch: | 106.2910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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