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 28500U 26145.53122647 +.00000000 +00000-0 +00000-0 0 00006
2 28500 13.9554 298.1055 2778809 23.7038 344.1469 1.41309965 07
| Epoch (UTC): | 25 May 2026 12:44:57 |
| Eccentricity: | 0.2778809 |
| inclination: | 13.9554° |
| perigee height: | 17845 km |
| apogee height: | 36488 km |
| right ascension of ascending node: | 298.1055° |
| argument of perigee: | 23.7038° |
| revolutions per day: | 1.41309965 |
| mean anomaly at epoch: | 344.1469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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