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 26069.81286598 +.00000000 +00000-0 +64019-3 0 00009
2 21965 19.6740 265.1587 1357284 114.1773 260.6278 12.22377084 07
| Epoch (UTC): | 10 March 2026 19:30:31 |
| Eccentricity: | 0.1357284 |
| inclination: | 19.6740° |
| perigee height: | 502 km |
| apogee height: | 2663 km |
| right ascension of ascending node: | 265.1587° |
| argument of perigee: | 114.1773° |
| revolutions per day: | 12.22377084 |
| mean anomaly at epoch: | 260.6278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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