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 58497U 26145.59337146 +.00000000 +00000-0 +13591-3 0 00004
2 58497 97.9268 227.7002 0010219 213.6100 146.4467 14.83177812 06
| Epoch (UTC): | 25 May 2026 14:14:27 |
| Eccentricity: | 0.0010219 |
| inclination: | 97.9268° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 227.7002° |
| argument of perigee: | 213.6100° |
| revolutions per day: | 14.83177812 |
| mean anomaly at epoch: | 146.4467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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