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 52156U 26145.57191352 +.00000000 +00000-0 +23154-3 0 00001
2 52156 97.5840 198.1159 0005401 222.3368 137.7445 15.10965664 08
| Epoch (UTC): | 25 May 2026 13:43:33 |
| Eccentricity: | 0.0005401 |
| inclination: | 97.5840° |
| perigee height: | 530 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 198.1159° |
| argument of perigee: | 222.3368° |
| revolutions per day: | 15.10965664 |
| mean anomaly at epoch: | 137.7445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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