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 43772U 26111.81388931 +.00000000 +00000-0 +11650-2 0 00003
2 43772 97.4211 189.3320 0001156 223.3138 136.8031 15.67104837 04
| Epoch (UTC): | 21 April 2026 19:32:00 |
| Eccentricity: | 0.0001156 |
| inclination: | 97.4211° |
| perigee height: | 366 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 189.3320° |
| argument of perigee: | 223.3138° |
| revolutions per day: | 15.67104837 |
| mean anomaly at epoch: | 136.8031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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