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 00082U 26048.12259184 +.00000000 +00000-0 +26783-3 0 00004
2 00082 38.8561 85.7565 1167056 4.7746 356.3036 12.27859883 02
| Epoch (UTC): | 17 February 2026 02:56:31 |
| Eccentricity: | 0.1167056 |
| inclination: | 38.8561° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 85.7565° |
| argument of perigee: | 4.7746° |
| revolutions per day: | 12.27859883 |
| mean anomaly at epoch: | 356.3036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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