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 52150U 26145.63616475 +.00000000 +00000-0 +21988-3 0 00003
2 52150 97.8315 341.5152 0015232 198.7153 161.3514 15.03394667 01
| Epoch (UTC): | 25 May 2026 15:16:04 |
| Eccentricity: | 0.0015232 |
| inclination: | 97.8315° |
| perigee height: | 546 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 341.5152° |
| argument of perigee: | 198.7153° |
| revolutions per day: | 15.03394667 |
| mean anomaly at epoch: | 161.3514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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