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 52693U 26145.47542809 +.00000000 +00000-0 +35054-5 0 00007
2 52693 53.2105 159.4152 0001005 30.4731 329.6319 15.08838111 03
| Epoch (UTC): | 25 May 2026 11:24:36 |
| Eccentricity: | 0.0001005 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 159.4152° |
| argument of perigee: | 30.4731° |
| revolutions per day: | 15.08838111 |
| mean anomaly at epoch: | 329.6319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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