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 53274U 26145.54534894 +.00000000 +00000-0 -11292-3 0 00003
2 53274 53.2107 199.1001 0001336 73.3194 286.7945 15.08842617 05
| Epoch (UTC): | 25 May 2026 13:05:18 |
| Eccentricity: | 0.0001336 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.1001° |
| argument of perigee: | 73.3194° |
| revolutions per day: | 15.08842617 |
| mean anomaly at epoch: | 286.7945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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