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 26103.87443079 +.00000000 +00000-0 +58035-4 0 00003
2 28380 82.9573 122.4710 0040649 72.9625 351.7470 13.76328947 05
| Epoch (UTC): | 13 April 2026 20:59:10 |
| Eccentricity: | 0.0040649 |
| inclination: | 82.9573° |
| perigee height: | 947 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 122.4710° |
| argument of perigee: | 72.9625° |
| revolutions per day: | 13.76328947 |
| mean anomaly at epoch: | 351.7470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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