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 58097U 26145.44477627 +.00000000 +00000-0 -14054-4 0 00000
2 58097 53.1589 168.9797 0001400 70.5743 289.5409 15.30193796 01
| Epoch (UTC): | 25 May 2026 10:40:28 |
| Eccentricity: | 0.0001400 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9797° |
| argument of perigee: | 70.5743° |
| revolutions per day: | 15.30193796 |
| mean anomaly at epoch: | 289.5409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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