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 53029U 26145.13962631 +.00000000 +00000-0 +14293-3 0 00003
2 53029 53.2132 90.9205 0001702 80.2244 279.8940 15.08845765 00
| Epoch (UTC): | 25 May 2026 03:21:03 |
| Eccentricity: | 0.0001702 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.9205° |
| argument of perigee: | 80.2244° |
| revolutions per day: | 15.08845765 |
| mean anomaly at epoch: | 279.8940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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