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 57984U 26145.64957703 +.00000000 +00000-0 +54384-4 0 00003
2 57984 43.0013 279.4386 0001540 254.6262 105.4419 15.27578001 02
| Epoch (UTC): | 25 May 2026 15:35:23 |
| Eccentricity: | 0.0001540 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 279.4386° |
| argument of perigee: | 254.6262° |
| revolutions per day: | 15.27578001 |
| mean anomaly at epoch: | 105.4419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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