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 53259U 26145.34934932 +.00000000 +00000-0 -29176-4 0 00002
2 53259 53.2138 209.6230 0001429 80.2411 279.8742 15.08837068 07
| Epoch (UTC): | 25 May 2026 08:23:03 |
| Eccentricity: | 0.0001429 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.6230° |
| argument of perigee: | 80.2411° |
| revolutions per day: | 15.08837068 |
| mean anomaly at epoch: | 279.8742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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