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 52374U 26145.45840919 +.00000000 +00000-0 -25681-4 0 00009
2 52374 53.2121 204.4925 0001435 81.0582 279.0572 15.08835396 00
| Epoch (UTC): | 25 May 2026 11:00:06 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.4925° |
| argument of perigee: | 81.0582° |
| revolutions per day: | 15.08835396 |
| mean anomaly at epoch: | 279.0572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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