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 53287U 26145.42390168 +.00000000 +00000-0 -36047-4 0 00004
2 53287 53.2135 199.6492 0001441 74.1921 285.9230 15.08837557 08
| Epoch (UTC): | 25 May 2026 10:10:25 |
| Eccentricity: | 0.0001441 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.6492° |
| argument of perigee: | 74.1921° |
| revolutions per day: | 15.08837557 |
| mean anomaly at epoch: | 285.9230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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