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 52546U 26145.29189242 +.00000000 +00000-0 -12868-3 0 00009
2 52546 53.2122 145.0064 0001246 84.8985 275.2150 15.08844748 05
| Epoch (UTC): | 25 May 2026 07:00:19 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 145.0064° |
| argument of perigee: | 84.8985° |
| revolutions per day: | 15.08844748 |
| mean anomaly at epoch: | 275.2150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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