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 26039.21223845 +.00000000 +00000-0 +70817-3 0 00004
2 00107 28.7795 339.8096 0495768 4.1023 356.3421 14.21443602 06
| Epoch (UTC): | 08 February 2026 05:05:37 |
| Eccentricity: | 0.0495768 |
| inclination: | 28.7795° |
| perigee height: | 464 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 339.8096° |
| argument of perigee: | 4.1023° |
| revolutions per day: | 14.21443602 |
| mean anomaly at epoch: | 356.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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