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 58972U 26145.43103314 +.00000000 +00000-0 -13217-3 0 00009
2 58972 53.1616 300.1630 0001544 100.2685 259.8490 15.30153712 09
| Epoch (UTC): | 25 May 2026 10:20:41 |
| Eccentricity: | 0.0001544 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.1630° |
| argument of perigee: | 100.2685° |
| revolutions per day: | 15.30153712 |
| mean anomaly at epoch: | 259.8490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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