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 21949U 26104.07652339 +.00000000 +00000-0 +45153-4 0 00008
2 21949 85.0033 111.0144 0001260 82.4953 277.6382 14.32379700 09
| Epoch (UTC): | 14 April 2026 01:50:11 |
| Eccentricity: | 0.0001260 |
| inclination: | 85.0033° |
| perigee height: | 783 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 111.0144° |
| argument of perigee: | 82.4953° |
| revolutions per day: | 14.32379700 |
| mean anomaly at epoch: | 277.6382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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