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 52448U 26145.60947926 +.00000000 +00000-0 +83874-3 0 00000
2 52448 97.5666 258.7696 0003024 180.3446 179.7816 15.74543635 04
| Epoch (UTC): | 25 May 2026 14:37:39 |
| Eccentricity: | 0.0003024 |
| inclination: | 97.5666° |
| perigee height: | 344 km |
| apogee height: | 348 km |
| right ascension of ascending node: | 258.7696° |
| argument of perigee: | 180.3446° |
| revolutions per day: | 15.74543635 |
| mean anomaly at epoch: | 179.7816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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