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 02680U 26053.22939200 +.00000000 +00000-0 +50138-3 0 00002
2 02680 39.4356 250.1140 0698924 107.0565 260.7893 13.41740764 05
| Epoch (UTC): | 22 February 2026 05:30:19 |
| Eccentricity: | 0.0698924 |
| inclination: | 39.4356° |
| perigee height: | 580 km |
| apogee height: | 1626 km |
| right ascension of ascending node: | 250.1140° |
| argument of perigee: | 107.0565° |
| revolutions per day: | 13.41740764 |
| mean anomaly at epoch: | 260.7893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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