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 26073.69760008 +.00000000 +00000-0 +85800-4 0 00008
2 28538 63.8245 166.1021 0214860 260.5117 97.1571 13.43369487 04
| Epoch (UTC): | 14 March 2026 16:44:32 |
| Eccentricity: | 0.0214860 |
| inclination: | 63.8245° |
| perigee height: | 936 km |
| apogee height: | 1257 km |
| right ascension of ascending node: | 166.1021° |
| argument of perigee: | 260.5117° |
| revolutions per day: | 13.43369487 |
| mean anomaly at epoch: | 97.1571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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