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 57234U 26144.95912272 +.00000000 +00000-0 -24787-5 0 00002
2 57234 43.0027 319.6607 0001444 252.3264 107.7430 15.27575044 00
| Epoch (UTC): | 24 May 2026 23:01:08 |
| Eccentricity: | 0.0001444 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 319.6607° |
| argument of perigee: | 252.3264° |
| revolutions per day: | 15.27575044 |
| mean anomaly at epoch: | 107.7430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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