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 57507U 26145.48925247 +.00000000 +00000-0 +51886-3 0 00007
2 57507 43.0022 302.0841 0002998 284.0135 76.0384 15.30117971 09
| Epoch (UTC): | 25 May 2026 11:44:31 |
| Eccentricity: | 0.0002998 |
| inclination: | 43.0022° |
| perigee height: | 473 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 302.0841° |
| argument of perigee: | 284.0135° |
| revolutions per day: | 15.30117971 |
| mean anomaly at epoch: | 76.0384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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