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 52443U 26145.55862963 +.00000000 +00000-0 +19533-3 0 00007
2 52443 97.5257 223.1473 0016292 47.4011 312.8589 15.10091185 01
| Epoch (UTC): | 25 May 2026 13:24:25 |
| Eccentricity: | 0.0016292 |
| inclination: | 97.5257° |
| perigee height: | 525 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 223.1473° |
| argument of perigee: | 47.4011° |
| revolutions per day: | 15.10091185 |
| mean anomaly at epoch: | 312.8589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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