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 26702U 26145.05170486 +.00000000 +00000-0 +10307-2 0 00002
2 26702 97.3902 184.6319 0004661 172.6884 187.4446 15.68405857 07
| Epoch (UTC): | 25 May 2026 01:14:27 |
| Eccentricity: | 0.0004661 |
| inclination: | 97.3902° |
| perigee height: | 360 km |
| apogee height: | 367 km |
| right ascension of ascending node: | 184.6319° |
| argument of perigee: | 172.6884° |
| revolutions per day: | 15.68405857 |
| mean anomaly at epoch: | 187.4446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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