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 52103U 26145.14468700 +.00000000 +00000-0 +46887-5 0 00000
2 52103 53.2131 95.9012 0001457 62.0714 298.0426 15.08838854 02
| Epoch (UTC): | 25 May 2026 03:28:20 |
| Eccentricity: | 0.0001457 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.9012° |
| argument of perigee: | 62.0714° |
| revolutions per day: | 15.08838854 |
| mean anomaly at epoch: | 298.0426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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