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 54843U 26144.95424441 +.00000000 +00000-0 +54575-5 0 00008
2 54843 43.0068 62.2358 0001143 267.8082 92.2639 15.27586425 01
| Epoch (UTC): | 24 May 2026 22:54:06 |
| Eccentricity: | 0.0001143 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.2358° |
| argument of perigee: | 267.8082° |
| revolutions per day: | 15.27586425 |
| mean anomaly at epoch: | 92.2639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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