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 25736U 26106.05325240 +.00000000 +00000-0 +14918-3 0 00008
2 25736 97.6932 330.6542 0005981 73.3460 286.8396 14.57071019 07
| Epoch (UTC): | 16 April 2026 01:16:41 |
| Eccentricity: | 0.0005981 |
| inclination: | 97.6932° |
| perigee height: | 698 km |
| apogee height: | 707 km |
| right ascension of ascending node: | 330.6542° |
| argument of perigee: | 73.3460° |
| revolutions per day: | 14.57071019 |
| mean anomaly at epoch: | 286.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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