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 28528U 26066.10454422 +.00000000 +00000-0 +16263-2 0 00000
2 28528 49.5136 209.4327 5012896 137.4261 274.8757 5.60250704 06
| Epoch (UTC): | 07 March 2026 02:30:32 |
| Eccentricity: | 0.5012896 |
| inclination: | 49.5136° |
| perigee height: | 300 km |
| apogee height: | 13726 km |
| right ascension of ascending node: | 209.4327° |
| argument of perigee: | 137.4261° |
| revolutions per day: | 5.60250704 |
| mean anomaly at epoch: | 274.8757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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