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 26039.80745677 +.00000000 +00000-0 +86157-4 0 00003
2 21949 85.0120 148.0948 0002601 103.4730 256.6752 14.32357253 02
| Epoch (UTC): | 08 February 2026 19:22:44 |
| Eccentricity: | 0.0002601 |
| inclination: | 85.0120° |
| perigee height: | 782 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 148.0948° |
| argument of perigee: | 103.4730° |
| revolutions per day: | 14.32357253 |
| mean anomaly at epoch: | 256.6752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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