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 21799U 26086.85506242 +.00000000 +00000-0 +73094-3 0 00001
2 21799 63.2983 2.6358 0884596 71.6616 297.8511 13.60579442 06
| Epoch (UTC): | 27 March 2026 20:31:17 |
| Eccentricity: | 0.0884596 |
| inclination: | 63.2983° |
| perigee height: | 378 km |
| apogee height: | 1689 km |
| right ascension of ascending node: | 2.6358° |
| argument of perigee: | 71.6616° |
| revolutions per day: | 13.60579442 |
| mean anomaly at epoch: | 297.8511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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