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 26105.99987762 +.00000000 +00000-0 +14457-3 0 00002
2 20624 71.0401 302.5300 0013896 154.5875 205.5934 14.14838959 04
| Epoch (UTC): | 15 April 2026 23:59:49 |
| Eccentricity: | 0.0013896 |
| inclination: | 71.0401° |
| perigee height: | 833 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 302.5300° |
| argument of perigee: | 154.5875° |
| revolutions per day: | 14.14838959 |
| mean anomaly at epoch: | 205.5934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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