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 26386U 26150.41230485 +.00000000 +00000-0 +23080-3 0 00005
2 26386 97.7558 137.8753 0009154 332.6942 27.3785 14.74852731 04
| Epoch (UTC): | 30 May 2026 09:53:43 |
| Eccentricity: | 0.0009154 |
| inclination: | 97.7558° |
| perigee height: | 639 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 137.8753° |
| argument of perigee: | 332.6942° |
| revolutions per day: | 14.74852731 |
| mean anomaly at epoch: | 27.3785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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