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 41789U 26150.81786171 +.00000000 +00000-0 +20108-3 0 00009
2 41789 97.8002 154.9422 0024411 242.4221 117.4506 14.69276448 08
| Epoch (UTC): | 30 May 2026 19:37:43 |
| Eccentricity: | 0.0024411 |
| inclination: | 97.8002° |
| perigee height: | 646 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 154.9422° |
| argument of perigee: | 242.4221° |
| revolutions per day: | 14.69276448 |
| mean anomaly at epoch: | 117.4506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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