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 54841U 26144.95167644 +.00000000 +00000-0 +62450-5 0 00006
2 54841 43.0066 62.2204 0001307 271.0290 89.0412 15.27574527 00
| Epoch (UTC): | 24 May 2026 22:50:24 |
| Eccentricity: | 0.0001307 |
| inclination: | 43.0066° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.2204° |
| argument of perigee: | 271.0290° |
| revolutions per day: | 15.27574527 |
| mean anomaly at epoch: | 89.0412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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