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 53502U 26145.66668980 +.00000000 +00000-0 +13652-1 0 00003
2 53502 97.6027 268.9282 0001432 86.2343 256.6338 15.42453345 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001432 |
| inclination: | 97.6027° |
| perigee height: | 438 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 268.9282° |
| argument of perigee: | 86.2343° |
| revolutions per day: | 15.42453345 |
| mean anomaly at epoch: | 256.6338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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