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 43784U 26145.40341623 +.00000000 +00000-0 +42824-3 0 00003
2 43784 97.3887 199.9151 0003268 43.0969 317.0525 15.26598846 02
| Epoch (UTC): | 25 May 2026 09:40:55 |
| Eccentricity: | 0.0003268 |
| inclination: | 97.3887° |
| perigee height: | 484 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 199.9151° |
| argument of perigee: | 43.0969° |
| revolutions per day: | 15.26598846 |
| mean anomaly at epoch: | 317.0525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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