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 52116U 26145.11894566 +.00000000 +00000-0 -51932-4 0 00001
2 52116 53.2134 96.0145 0001230 104.9011 255.2118 15.08832950 07
| Epoch (UTC): | 25 May 2026 02:51:16 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 96.0145° |
| argument of perigee: | 104.9011° |
| revolutions per day: | 15.08832950 |
| mean anomaly at epoch: | 255.2118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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