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 55284U 26145.62076579 +.00000000 +00000-0 +14777-1 0 00004
2 55284 69.9994 210.3099 0003745 270.9278 89.1452 14.98789315 04
| Epoch (UTC): | 25 May 2026 14:53:54 |
| Eccentricity: | 0.0003745 |
| inclination: | 69.9994° |
| perigee height: | 568 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 210.3099° |
| argument of perigee: | 270.9278° |
| revolutions per day: | 14.98789315 |
| mean anomaly at epoch: | 89.1452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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