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 57915U 26145.34552303 +.00000000 +00000-0 -17214-3 0 00002
2 57915 43.0017 252.1190 0001010 281.1927 78.8811 15.27573231 05
| Epoch (UTC): | 25 May 2026 08:17:33 |
| Eccentricity: | 0.0001010 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.1190° |
| argument of perigee: | 281.1927° |
| revolutions per day: | 15.27573231 |
| mean anomaly at epoch: | 78.8811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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