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 20103U 26053.67629192 +.00000000 +00000-0 +57054-4 0 00002
2 20103 82.9614 26.0505 0038823 68.0976 117.9122 13.74839886 06
| Epoch (UTC): | 22 February 2026 16:13:51 |
| Eccentricity: | 0.0038823 |
| inclination: | 82.9614° |
| perigee height: | 954 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 26.0505° |
| argument of perigee: | 68.0976° |
| revolutions per day: | 13.74839886 |
| mean anomaly at epoch: | 117.9122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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