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 26156.48006096 +.00000000 +00000-0 -41361-4 0 00000
2 20624 71.0398 196.7645 0012615 65.9022 294.3419 14.14846614 02
| Epoch (UTC): | 05 June 2026 11:31:17 |
| Eccentricity: | 0.0012615 |
| inclination: | 71.0398° |
| perigee height: | 834 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 196.7645° |
| argument of perigee: | 65.9022° |
| revolutions per day: | 14.14846614 |
| mean anomaly at epoch: | 294.3419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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