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 52830U 26145.42302034 +.00000000 +00000-0 +34527-3 0 00001
2 52830 53.2135 49.8425 0001317 93.2105 266.9038 15.08807460 06
| Epoch (UTC): | 25 May 2026 10:09:08 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.8425° |
| argument of perigee: | 93.2105° |
| revolutions per day: | 15.08807460 |
| mean anomaly at epoch: | 266.9038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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