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 52832U 26145.54438470 +.00000000 +00000-0 +42930-3 0 00007
2 52832 53.2157 49.1033 0001363 212.1883 147.9026 15.08879308 01
| Epoch (UTC): | 25 May 2026 13:03:54 |
| Eccentricity: | 0.0001363 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.1033° |
| argument of perigee: | 212.1883° |
| revolutions per day: | 15.08879308 |
| mean anomaly at epoch: | 147.9026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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