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 55283U 26145.44121809 +.00000000 +00000-0 -45838-4 0 00006
2 55283 69.9997 210.8922 0003406 265.2152 94.8618 14.98333774 09
| Epoch (UTC): | 25 May 2026 10:35:21 |
| Eccentricity: | 0.0003406 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 210.8922° |
| argument of perigee: | 265.2152° |
| revolutions per day: | 14.98333774 |
| mean anomaly at epoch: | 94.8618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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