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 20624U 26042.08609203 +.00000000 +00000-0 -97784-4 0 00009
2 20624 71.0389 76.4410 0017203 248.4867 111.4422 14.14824300 00
| Epoch (UTC): | 11 February 2026 02:03:58 |
| Eccentricity: | 0.0017203 |
| inclination: | 71.0389° |
| perigee height: | 830 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 76.4410° |
| argument of perigee: | 248.4867° |
| revolutions per day: | 14.14824300 |
| mean anomaly at epoch: | 111.4422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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