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 52899U 26145.34497987 +.00000000 +00000-0 +17489-3 0 00007
2 52899 98.2174 290.2207 0008798 95.8254 264.3951 14.64296892 04
| Epoch (UTC): | 25 May 2026 08:16:46 |
| Eccentricity: | 0.0008798 |
| inclination: | 98.2174° |
| perigee height: | 673 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 290.2207° |
| argument of perigee: | 95.8254° |
| revolutions per day: | 14.64296892 |
| mean anomaly at epoch: | 264.3951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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