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 54207U 26145.33094616 +.00000000 +00000-0 +56987-4 0 00000
2 54207 53.2146 9.6707 0001368 90.7354 269.3795 15.08829220 04
| Epoch (UTC): | 25 May 2026 07:56:33 |
| Eccentricity: | 0.0001368 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.6707° |
| argument of perigee: | 90.7354° |
| revolutions per day: | 15.08829220 |
| mean anomaly at epoch: | 269.3795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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