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 57376U 26145.47440669 +.00000000 +00000-0 +58470-3 0 00006
2 57376 43.0025 164.5318 0001482 262.5488 97.5195 15.27592965 09
| Epoch (UTC): | 25 May 2026 11:23:08 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5318° |
| argument of perigee: | 262.5488° |
| revolutions per day: | 15.27592965 |
| mean anomaly at epoch: | 97.5195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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