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 26042.09182387 +.00000000 +00000-0 +65800-3 0 00005
2 00107 28.7777 323.2243 0495718 30.9784 331.9077 14.21474658 04
| Epoch (UTC): | 11 February 2026 02:12:13 |
| Eccentricity: | 0.0495718 |
| inclination: | 28.7777° |
| perigee height: | 464 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 323.2243° |
| argument of perigee: | 30.9784° |
| revolutions per day: | 14.21474658 |
| mean anomaly at epoch: | 331.9077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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