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 51864U 26144.95239758 +.00000000 +00000-0 -12444-4 0 00002
2 51864 53.2172 26.6862 0001352 93.4693 266.6454 15.08838315 06
| Epoch (UTC): | 24 May 2026 22:51:27 |
| Eccentricity: | 0.0001352 |
| inclination: | 53.2172° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.6862° |
| argument of perigee: | 93.4693° |
| revolutions per day: | 15.08838315 |
| mean anomaly at epoch: | 266.6454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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