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 53978U 26145.52923414 +.00000000 +00000-0 +24920-4 0 00004
2 53978 53.2116 234.0887 0001391 89.6954 270.4197 15.08855339 06
| Epoch (UTC): | 25 May 2026 12:42:05 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.0887° |
| argument of perigee: | 89.6954° |
| revolutions per day: | 15.08855339 |
| mean anomaly at epoch: | 270.4197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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