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 53282U 26145.45334951 +.00000000 +00000-0 +24981-4 0 00003
2 53282 53.2126 199.5162 0001389 95.4050 264.7100 15.08836131 04
| Epoch (UTC): | 25 May 2026 10:52:49 |
| Eccentricity: | 0.0001389 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.5162° |
| argument of perigee: | 95.4050° |
| revolutions per day: | 15.08836131 |
| mean anomaly at epoch: | 264.7100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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