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 20843U 26103.08286713 +.00000000 +00000-0 +78548-3 0 00002
2 20843 28.1830 91.2212 6684459 114.4890 326.5658 3.03727372 06
| Epoch (UTC): | 13 April 2026 01:59:19 |
| Eccentricity: | 0.6684459 |
| inclination: | 28.1830° |
| perigee height: | 300 km |
| apogee height: | 27226 km |
| right ascension of ascending node: | 91.2212° |
| argument of perigee: | 114.4890° |
| revolutions per day: | 3.03727372 |
| mean anomaly at epoch: | 326.5658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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