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 43162U 26140.56151516 +.00000000 +00000-0 +00000-0 0 00002
2 43162 2.1663 10.8113 0001991 36.4090 233.7440 1.00271868 08
| Epoch (UTC): | 20 May 2026 13:28:34 |
| Eccentricity: | 0.0001991 |
| inclination: | 2.1663° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 10.8113° |
| argument of perigee: | 36.4090° |
| revolutions per day: | 1.00271868 |
| mean anomaly at epoch: | 233.7440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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