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 53970U 26145.54029425 +.00000000 +00000-0 +36003-4 0 00002
2 53970 53.2151 234.1651 0001458 89.1302 270.9858 15.08835975 06
| Epoch (UTC): | 25 May 2026 12:58:01 |
| Eccentricity: | 0.0001458 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.1651° |
| argument of perigee: | 89.1302° |
| revolutions per day: | 15.08835975 |
| mean anomaly at epoch: | 270.9858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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