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 58368U 26144.85390868 +.00000000 +00000-0 +38617-4 0 00006
2 58368 42.9982 280.6496 0002640 245.7622 114.2954 15.27578092 03
| Epoch (UTC): | 24 May 2026 20:29:37 |
| Eccentricity: | 0.0002640 |
| inclination: | 42.9982° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 280.6496° |
| argument of perigee: | 245.7622° |
| revolutions per day: | 15.27578092 |
| mean anomaly at epoch: | 114.2954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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