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 26040.29646448 +.00000000 +00000-0 +87070-4 0 00009
2 21949 85.0120 147.8129 0002622 102.9819 257.1666 14.32357539 02
| Epoch (UTC): | 09 February 2026 07:06:54 |
| Eccentricity: | 0.0002622 |
| inclination: | 85.0120° |
| perigee height: | 782 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 147.8129° |
| argument of perigee: | 102.9819° |
| revolutions per day: | 14.32357539 |
| mean anomaly at epoch: | 257.1666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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