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 25501U 26140.54747509 +.00000000 +00000-0 +00000-0 0 00000
2 25501 11.2742 21.4467 0012640 353.3855 190.5095 0.98177708 07
| Epoch (UTC): | 20 May 2026 13:08:21 |
| Eccentricity: | 0.0012640 |
| inclination: | 11.2742° |
| perigee height: | 36330 km |
| apogee height: | 36438 km |
| right ascension of ascending node: | 21.4467° |
| argument of perigee: | 353.3855° |
| revolutions per day: | 0.98177708 |
| mean anomaly at epoch: | 190.5095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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