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 51463U 26145.38020859 +.00000000 +00000-0 +49727-4 0 00008
2 51463 53.2140 294.8413 0001446 100.8875 259.2280 15.08838321 08
| Epoch (UTC): | 25 May 2026 09:07:30 |
| Eccentricity: | 0.0001446 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.8413° |
| argument of perigee: | 100.8875° |
| revolutions per day: | 15.08838321 |
| mean anomaly at epoch: | 259.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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