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 12339U 26150.35030505 +.00000000 +00000-0 +00000-0 0 00006
2 12339 8.1339 305.1571 0017889 292.0794 85.3225 0.98829056 04
| Epoch (UTC): | 30 May 2026 08:24:26 |
| Eccentricity: | 0.0017889 |
| inclination: | 8.1339° |
| perigee height: | 36120 km |
| apogee height: | 36272 km |
| right ascension of ascending node: | 305.1571° |
| argument of perigee: | 292.0794° |
| revolutions per day: | 0.98829056 |
| mean anomaly at epoch: | 85.3225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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