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 57981U 26145.37644910 +.00000000 +00000-0 +62004-3 0 00000
2 57981 43.0066 280.8369 0004444 292.3249 67.7132 15.27623713 07
| Epoch (UTC): | 25 May 2026 09:02:05 |
| Eccentricity: | 0.0004444 |
| inclination: | 43.0066° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 280.8369° |
| argument of perigee: | 292.3249° |
| revolutions per day: | 15.27623713 |
| mean anomaly at epoch: | 67.7132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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