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 54752U 26145.63503112 +.00000000 +00000-0 +23742-3 0 00006
2 54752 35.9794 212.9320 0019275 50.3099 309.9331 15.28467007 09
| Epoch (UTC): | 25 May 2026 15:14:26 |
| Eccentricity: | 0.0019275 |
| inclination: | 35.9794° |
| perigee height: | 467 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 212.9320° |
| argument of perigee: | 50.3099° |
| revolutions per day: | 15.28467007 |
| mean anomaly at epoch: | 309.9331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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