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 52350U 26145.46852625 +.00000000 +00000-0 +60595-4 0 00003
2 52350 53.2117 214.4478 0001189 71.8568 288.2554 15.08838938 07
| Epoch (UTC): | 25 May 2026 11:14:40 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.4478° |
| argument of perigee: | 71.8568° |
| revolutions per day: | 15.08838938 |
| mean anomaly at epoch: | 288.2554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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