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 57765U 26145.38255382 +.00000000 +00000-0 -15335-4 0 00009
2 57765 81.0047 29.8451 0007012 74.7321 285.4610 13.85387153 05
| Epoch (UTC): | 25 May 2026 09:10:52 |
| Eccentricity: | 0.0007012 |
| inclination: | 81.0047° |
| perigee height: | 940 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 29.8451° |
| argument of perigee: | 74.7321° |
| revolutions per day: | 13.85387153 |
| mean anomaly at epoch: | 285.4610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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