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 53285U 26145.56374382 +.00000000 +00000-0 -78661-5 0 00006
2 53285 53.2102 199.0204 0001279 85.2621 274.8517 15.08833179 05
| Epoch (UTC): | 25 May 2026 13:31:47 |
| Eccentricity: | 0.0001279 |
| inclination: | 53.2102° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.0204° |
| argument of perigee: | 85.2621° |
| revolutions per day: | 15.08833179 |
| mean anomaly at epoch: | 274.8517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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