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 26039.07176808 +.00000000 +00000-0 +69187-3 0 00002
2 00107 28.7796 340.6186 0495770 2.7908 357.5285 14.21441764 04
| Epoch (UTC): | 08 February 2026 01:43:20 |
| Eccentricity: | 0.0495770 |
| inclination: | 28.7796° |
| perigee height: | 464 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 340.6186° |
| argument of perigee: | 2.7908° |
| revolutions per day: | 14.21441764 |
| mean anomaly at epoch: | 357.5285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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