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 25515U 26113.48655807 +.00000000 +00000-0 +00000-0 0 00007
2 25515 10.1098 50.2721 0001363 323.2033 248.9869 0.99006054 04
| Epoch (UTC): | 23 April 2026 11:40:38 |
| Eccentricity: | 0.0001363 |
| inclination: | 10.1098° |
| perigee height: | 36139 km |
| apogee height: | 36151 km |
| right ascension of ascending node: | 50.2721° |
| argument of perigee: | 323.2033° |
| revolutions per day: | 0.99006054 |
| mean anomaly at epoch: | 248.9869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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