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 45428U 26145.12697588 +.00000000 +00000-0 +11444-2 0 00006
2 45428 87.8916 25.6433 0001777 80.1651 279.9678 13.11415047 05
| Epoch (UTC): | 25 May 2026 03:02:50 |
| Eccentricity: | 0.0001777 |
| inclination: | 87.8916° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6433° |
| argument of perigee: | 80.1651° |
| revolutions per day: | 13.11415047 |
| mean anomaly at epoch: | 279.9678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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