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 26041.03833205 +.00000000 +00000-0 +66246-3 0 00005
2 00107 28.7785 329.2914 0495674 21.1466 340.8863 14.21463238 08
| Epoch (UTC): | 10 February 2026 00:55:11 |
| Eccentricity: | 0.0495674 |
| inclination: | 28.7785° |
| perigee height: | 464 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 329.2914° |
| argument of perigee: | 21.1466° |
| revolutions per day: | 14.21463238 |
| mean anomaly at epoch: | 340.8863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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