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 21798U 26140.60510053 +.00000000 +00000-0 +35873-4 0 00003
2 21798 98.6921 169.4644 0012253 356.1679 3.9400 14.17442779 00
| Epoch (UTC): | 20 May 2026 14:31:20 |
| Eccentricity: | 0.0012253 |
| inclination: | 98.6921° |
| perigee height: | 825 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 169.4644° |
| argument of perigee: | 356.1679° |
| revolutions per day: | 14.17442779 |
| mean anomaly at epoch: | 3.9400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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