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 24954U 26150.54756169 +.00000000 +00000-0 +81487-4 0 00006
2 24954 82.9231 357.3923 0039420 3.4766 15.7385 13.80370818 05
| Epoch (UTC): | 30 May 2026 13:08:29 |
| Eccentricity: | 0.0039420 |
| inclination: | 82.9231° |
| perigee height: | 934 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 357.3923° |
| argument of perigee: | 3.4766° |
| revolutions per day: | 13.80370818 |
| mean anomaly at epoch: | 15.7385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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