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 26041.24903196 +.00000000 +00000-0 +65409-3 0 00005
2 00107 28.7784 328.0779 0495657 23.1130 339.0953 14.21465414 02
| Epoch (UTC): | 10 February 2026 05:58:36 |
| Eccentricity: | 0.0495657 |
| inclination: | 28.7784° |
| perigee height: | 464 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 328.0779° |
| argument of perigee: | 23.1130° |
| revolutions per day: | 14.21465414 |
| mean anomaly at epoch: | 339.0953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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