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 54870U 26145.11959287 +.00000000 +00000-0 +25494-4 0 00005
2 54870 43.0056 49.5949 0001335 285.4094 74.6610 15.27571138 02
| Epoch (UTC): | 25 May 2026 02:52:12 |
| Eccentricity: | 0.0001335 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.5949° |
| argument of perigee: | 285.4094° |
| revolutions per day: | 15.27571138 |
| mean anomaly at epoch: | 74.6610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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