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 25078U 26088.09606314 +.00000000 +00000-0 +10997-3 0 00007
2 25078 86.3898 101.0462 0003113 127.0056 233.1428 14.40523908 08
| Epoch (UTC): | 29 March 2026 02:18:19 |
| Eccentricity: | 0.0003113 |
| inclination: | 86.3898° |
| perigee height: | 755 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 101.0462° |
| argument of perigee: | 127.0056° |
| revolutions per day: | 14.40523908 |
| mean anomaly at epoch: | 233.1428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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