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 28538U 26040.79464771 +.00000000 +00000-0 +82251-4 0 00008
2 28538 63.8219 249.1449 0215136 262.3962 95.2586 13.43365465 03
| Epoch (UTC): | 09 February 2026 19:04:17 |
| Eccentricity: | 0.0215136 |
| inclination: | 63.8219° |
| perigee height: | 936 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 249.1449° |
| argument of perigee: | 262.3962° |
| revolutions per day: | 13.43365465 |
| mean anomaly at epoch: | 95.2586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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