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 53681U 26145.50003470 +.00000000 +00000-0 +12081-1 0 00006
2 53681 97.6034 27.8642 0001388 84.9339 193.3089 15.45271130 01
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001388 |
| inclination: | 97.6034° |
| perigee height: | 430 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 27.8642° |
| argument of perigee: | 84.9339° |
| revolutions per day: | 15.45271130 |
| mean anomaly at epoch: | 193.3089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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