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 68036U 26145.34565389 +.00000000 +00000-0 +69882-3 0 00003
2 68036 97.2846 94.3967 0000904 67.8810 292.2529 15.33457297 09
| Epoch (UTC): | 25 May 2026 08:17:44 |
| Eccentricity: | 0.0000904 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 94.3967° |
| argument of perigee: | 67.8810° |
| revolutions per day: | 15.33457297 |
| mean anomaly at epoch: | 292.2529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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