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 65884U 26145.37272199 +.00000000 +00000-0 +46962-3 0 00002
2 65884 53.1605 15.2461 0001230 96.2132 263.9009 15.30204964 04
| Epoch (UTC): | 25 May 2026 08:56:43 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 15.2461° |
| argument of perigee: | 96.2132° |
| revolutions per day: | 15.30204964 |
| mean anomaly at epoch: | 263.9009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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