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 52445U 26145.60556322 +.00000000 +00000-0 +84225-3 0 00004
2 52445 97.5628 257.6651 0003736 157.0511 203.0920 15.72405649 09
| Epoch (UTC): | 25 May 2026 14:32:00 |
| Eccentricity: | 0.0003736 |
| inclination: | 97.5628° |
| perigee height: | 350 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 257.6651° |
| argument of perigee: | 157.0511° |
| revolutions per day: | 15.72405649 |
| mean anomaly at epoch: | 203.0920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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