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 65897U 26145.33395172 +.00000000 +00000-0 +66780-3 0 00009
2 65897 53.1590 14.2887 0001103 71.9676 288.1446 15.34404324 04
| Epoch (UTC): | 25 May 2026 08:00:53 |
| Eccentricity: | 0.0001103 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 14.2887° |
| argument of perigee: | 71.9676° |
| revolutions per day: | 15.34404324 |
| mean anomaly at epoch: | 288.1446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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