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 57913U 26145.33780222 +.00000000 +00000-0 +12596-3 0 00009
2 57913 43.0035 252.0624 0001707 267.1737 92.8920 15.27579328 00
| Epoch (UTC): | 25 May 2026 08:06:26 |
| Eccentricity: | 0.0001707 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.0624° |
| argument of perigee: | 267.1737° |
| revolutions per day: | 15.27579328 |
| mean anomaly at epoch: | 92.8920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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