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 21965U 26161.50430913 +.00000000 +00000-0 +11621-3 0 00001
2 21965 19.6748 212.7879 1357128 145.8971 223.6529 12.22506602 03
| Epoch (UTC): | 10 June 2026 12:06:12 |
| Eccentricity: | 0.1357128 |
| inclination: | 19.6748° |
| perigee height: | 501 km |
| apogee height: | 2662 km |
| right ascension of ascending node: | 212.7879° |
| argument of perigee: | 145.8971° |
| revolutions per day: | 12.22506602 |
| mean anomaly at epoch: | 223.6529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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