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 28380U 26106.80425730 +.00000000 +00000-0 +40077-4 0 00000
2 28380 82.9570 120.3005 0040569 65.0273 108.1466 13.76329162 08
| Epoch (UTC): | 16 April 2026 19:18:07 |
| Eccentricity: | 0.0040569 |
| inclination: | 82.9570° |
| perigee height: | 947 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 120.3005° |
| argument of perigee: | 65.0273° |
| revolutions per day: | 13.76329162 |
| mean anomaly at epoch: | 108.1466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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