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 25615U 26146.13748082 +.00000000 +00000-0 +78746-4 0 00000
2 25615 84.9866 20.9867 0005740 286.7533 73.3038 14.47232210 04
| Epoch (UTC): | 26 May 2026 03:17:58 |
| Eccentricity: | 0.0005740 |
| inclination: | 84.9866° |
| perigee height: | 731 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 20.9867° |
| argument of perigee: | 286.7533° |
| revolutions per day: | 14.47232210 |
| mean anomaly at epoch: | 73.3038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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