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 52096U 26145.54950237 +.00000000 +00000-0 -78010-4 0 00009
2 52096 53.2126 94.0806 0001217 83.2866 276.8264 15.08830820 04
| Epoch (UTC): | 25 May 2026 13:11:17 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 94.0806° |
| argument of perigee: | 83.2866° |
| revolutions per day: | 15.08830820 |
| mean anomaly at epoch: | 276.8264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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