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 65797U 26145.57861147 +.00000000 +00000-0 +87525-4 0 00005
2 65797 97.4484 8.4221 0002275 62.8475 297.2984 15.05665117 05
| Epoch (UTC): | 25 May 2026 13:53:12 |
| Eccentricity: | 0.0002275 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.4221° |
| argument of perigee: | 62.8475° |
| revolutions per day: | 15.05665117 |
| mean anomaly at epoch: | 297.2984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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