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 20217U 26106.73667985 +.00000000 +00000-0 +00000-0 0 00001
2 20217 14.8251 347.2734 0043710 144.1072 33.7489 0.97410890 01
| Epoch (UTC): | 16 April 2026 17:40:49 |
| Eccentricity: | 0.0043710 |
| inclination: | 14.8251° |
| perigee height: | 36420 km |
| apogee height: | 36796 km |
| right ascension of ascending node: | 347.2734° |
| argument of perigee: | 144.1072° |
| revolutions per day: | 0.97410890 |
| mean anomaly at epoch: | 33.7489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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