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 57941U 26145.35119334 +.00000000 +00000-0 -26258-6 0 00006
2 57941 53.1612 17.9006 0001092 101.4423 258.6700 15.30193465 01
| Epoch (UTC): | 25 May 2026 08:25:43 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 17.9006° |
| argument of perigee: | 101.4423° |
| revolutions per day: | 15.30193465 |
| mean anomaly at epoch: | 258.6700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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