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 53675U 26145.62268819 +.00000000 +00000-0 -45968-4 0 00006
2 53675 97.4510 26.7274 0002479 82.2341 277.9167 15.05659922 07
| Epoch (UTC): | 25 May 2026 14:56:40 |
| Eccentricity: | 0.0002479 |
| inclination: | 97.4510° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.7274° |
| argument of perigee: | 82.2341° |
| revolutions per day: | 15.05659922 |
| mean anomaly at epoch: | 277.9167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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