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 53499U 26145.66668980 +.00000000 +00000-0 -21884-1 0 00005
2 53499 97.6015 268.3327 0001205 79.5754 315.7380 15.32414750 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001205 |
| inclination: | 97.6015° |
| perigee height: | 468 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 268.3327° |
| argument of perigee: | 79.5754° |
| revolutions per day: | 15.32414750 |
| mean anomaly at epoch: | 315.7380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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