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 52155U 26145.57247492 +.00000000 +00000-0 +10364-3 0 00006
2 52155 97.5902 191.3426 0020888 234.6564 125.2708 15.01574846 00
| Epoch (UTC): | 25 May 2026 13:44:21 |
| Eccentricity: | 0.0020888 |
| inclination: | 97.5902° |
| perigee height: | 548 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 191.3426° |
| argument of perigee: | 234.6564° |
| revolutions per day: | 15.01574846 |
| mean anomaly at epoch: | 125.2708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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