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 00020U 26039.33437481 +.00000000 +00000-0 +47641-3 0 00003
2 00020 33.3449 10.8439 1638320 82.7978 295.5202 11.61810304 09
| Epoch (UTC): | 08 February 2026 08:01:29 |
| Eccentricity: | 0.1638320 |
| inclination: | 33.3449° |
| perigee height: | 507 km |
| apogee height: | 3206 km |
| right ascension of ascending node: | 10.8439° |
| argument of perigee: | 82.7978° |
| revolutions per day: | 11.61810304 |
| mean anomaly at epoch: | 295.5202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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