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 57077U 26145.04466646 +.00000000 +00000-0 +12688-4 0 00002
2 57077 43.0037 25.2799 0000933 266.5837 93.4908 15.27575244 06
| Epoch (UTC): | 25 May 2026 01:04:19 |
| Eccentricity: | 0.0000933 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.2799° |
| argument of perigee: | 266.5837° |
| revolutions per day: | 15.27575244 |
| mean anomaly at epoch: | 93.4908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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