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 65893U 26145.05669918 +.00000000 +00000-0 +34959-3 0 00009
2 65893 53.1596 16.8239 0001229 88.8548 271.2594 15.30204917 08
| Epoch (UTC): | 25 May 2026 01:21:38 |
| Eccentricity: | 0.0001229 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 16.8239° |
| argument of perigee: | 88.8548° |
| revolutions per day: | 15.30204917 |
| mean anomaly at epoch: | 271.2594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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