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 26047.00774853 +.00000000 +00000-0 +66497-3 0 00009
2 00107 28.7761 294.9075 0495637 76.8275 288.7103 14.21526217 06
| Epoch (UTC): | 16 February 2026 00:11:09 |
| Eccentricity: | 0.0495637 |
| inclination: | 28.7761° |
| perigee height: | 463 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 294.9075° |
| argument of perigee: | 76.8275° |
| revolutions per day: | 14.21526217 |
| mean anomaly at epoch: | 288.7103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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