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 28359U 26064.25320057 +.00000000 +00000-0 +84628-3 0 00003
2 28359 49.5285 28.7624 4501441 124.6650 286.3785 6.50540474 08
| Epoch (UTC): | 05 March 2026 06:04:36 |
| Eccentricity: | 0.4501441 |
| inclination: | 49.5285° |
| perigee height: | 287 km |
| apogee height: | 11200 km |
| right ascension of ascending node: | 28.7624° |
| argument of perigee: | 124.6650° |
| revolutions per day: | 6.50540474 |
| mean anomaly at epoch: | 286.3785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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