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 52359U 26145.45108561 +.00000000 +00000-0 +47404-4 0 00008
2 52359 53.2127 214.5374 0001028 88.7528 271.3582 15.08838224 00
| Epoch (UTC): | 25 May 2026 10:49:33 |
| Eccentricity: | 0.0001028 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 214.5374° |
| argument of perigee: | 88.7528° |
| revolutions per day: | 15.08838224 |
| mean anomaly at epoch: | 271.3582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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