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 26158.78330328 +.00000000 +00000-0 +11611-3 0 00008
2 28538 63.8253 311.3547 0213348 255.6660 102.0599 13.43378054 04
| Epoch (UTC): | 07 June 2026 18:47:57 |
| Eccentricity: | 0.0213348 |
| inclination: | 63.8253° |
| perigee height: | 937 km |
| apogee height: | 1256 km |
| right ascension of ascending node: | 311.3547° |
| argument of perigee: | 255.6660° |
| revolutions per day: | 13.43378054 |
| mean anomaly at epoch: | 102.0599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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