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 52817U 26145.58225508 +.00000000 +00000-0 +00000-0 0 00009
2 52817 0.0646 37.7222 0005793 359.4813 48.5551 1.00271828 08
| Epoch (UTC): | 25 May 2026 13:58:26 |
| Eccentricity: | 0.0005793 |
| inclination: | 0.0646° |
| perigee height: | 35762 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 37.7222° |
| argument of perigee: | 359.4813° |
| revolutions per day: | 1.00271828 |
| mean anomaly at epoch: | 48.5551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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