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 00029U 26039.00098440 +.00000000 +00000-0 +13849-3 0 00007
2 00029 48.3779 278.5135 0021891 72.0271 288.3027 14.78565253 08
| Epoch (UTC): | 08 February 2026 00:01:25 |
| Eccentricity: | 0.0021891 |
| inclination: | 48.3779° |
| perigee height: | 619 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 278.5135° |
| argument of perigee: | 72.0271° |
| revolutions per day: | 14.78565253 |
| mean anomaly at epoch: | 288.3027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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