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 53917U 26145.50003470 +.00000000 +00000-0 +12442-1 0 00009
2 53917 53.2167 322.2192 0001108 79.3854 217.7257 15.45706840 09
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001108 |
| inclination: | 53.2167° |
| perigee height: | 429 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 322.2192° |
| argument of perigee: | 79.3854° |
| revolutions per day: | 15.45706840 |
| mean anomaly at epoch: | 217.7257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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