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 52839U 26145.11386992 +.00000000 +00000-0 +52019-4 0 00008
2 52839 53.2123 51.0400 0001396 96.9690 263.1461 15.08835073 06
| Epoch (UTC): | 25 May 2026 02:43:58 |
| Eccentricity: | 0.0001396 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 51.0400° |
| argument of perigee: | 96.9690° |
| revolutions per day: | 15.08835073 |
| mean anomaly at epoch: | 263.1461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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