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 26162.13312492 +.00000000 +00000-0 +60743-4 0 00005
2 28538 63.8254 302.9003 0213287 255.4720 102.2566 13.43378178 08
| Epoch (UTC): | 11 June 2026 03:11:41 |
| Eccentricity: | 0.0213287 |
| inclination: | 63.8254° |
| perigee height: | 937 km |
| apogee height: | 1256 km |
| right ascension of ascending node: | 302.9003° |
| argument of perigee: | 255.4720° |
| revolutions per day: | 13.43378178 |
| mean anomaly at epoch: | 102.2566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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