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 68013U 26145.25178280 +.00000000 +00000-0 +69566-3 0 00007
2 68013 43.0044 336.4688 0001768 276.8210 83.2441 15.27595341 05
| Epoch (UTC): | 25 May 2026 06:02:34 |
| Eccentricity: | 0.0001768 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 336.4688° |
| argument of perigee: | 276.8210° |
| revolutions per day: | 15.27595341 |
| mean anomaly at epoch: | 83.2441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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