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 26106.91329881 +.00000000 +00000-0 +53041-4 0 00002
2 20103 82.9634 346.7385 0036095 279.3797 91.2466 13.74846732 06
| Epoch (UTC): | 16 April 2026 21:55:09 |
| Eccentricity: | 0.0036095 |
| inclination: | 82.9634° |
| perigee height: | 956 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 346.7385° |
| argument of perigee: | 279.3797° |
| revolutions per day: | 13.74846732 |
| mean anomaly at epoch: | 91.2466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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