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 26073.07981730 +.00000000 +00000-0 +89853-3 0 00003
2 65893 53.1607 351.1512 0001307 63.1381 296.9754 15.30199615 08
| Epoch (UTC): | 14 March 2026 01:54:56 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.1512° |
| argument of perigee: | 63.1381° |
| revolutions per day: | 15.30199615 |
| mean anomaly at epoch: | 296.9754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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