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 58028U 26145.53098500 +.00000000 +00000-0 +18340-4 0 00004
2 58028 53.1611 81.2480 0001738 94.6808 265.4391 15.30192342 09
| Epoch (UTC): | 25 May 2026 12:44:37 |
| Eccentricity: | 0.0001738 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.2480° |
| argument of perigee: | 94.6808° |
| revolutions per day: | 15.30192342 |
| mean anomaly at epoch: | 265.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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