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 26140.39878912 +.00000000 +00000-0 +55014-4 0 00001
2 25615 84.9871 24.3937 0006068 311.0833 48.9843 14.47229089 07
| Epoch (UTC): | 20 May 2026 09:34:15 |
| Eccentricity: | 0.0006068 |
| inclination: | 84.9871° |
| perigee height: | 730 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 24.3937° |
| argument of perigee: | 311.0833° |
| revolutions per day: | 14.47229089 |
| mean anomaly at epoch: | 48.9843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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