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 26140.19993667 +.00000000 +00000-0 +00000-0 0 00001
2 28500 13.9662 298.2906 2779026 23.3433 152.0704 1.41309972 06
| Epoch (UTC): | 20 May 2026 04:47:54 |
| Eccentricity: | 0.2779026 |
| inclination: | 13.9662° |
| perigee height: | 17844 km |
| apogee height: | 36488 km |
| right ascension of ascending node: | 298.2906° |
| argument of perigee: | 23.3433° |
| revolutions per day: | 1.41309972 |
| mean anomaly at epoch: | 152.0704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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