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 04793U 26133.33571396 +.00000000 +00000-0 +42413-4 0 00006
2 04793 101.3392 169.6075 0031927 55.5683 315.8211 12.54050071 08
| Epoch (UTC): | 13 May 2026 08:03:25 |
| Eccentricity: | 0.0031927 |
| inclination: | 101.3392° |
| perigee height: | 1423 km |
| apogee height: | 1473 km |
| right ascension of ascending node: | 169.6075° |
| argument of perigee: | 55.5683° |
| revolutions per day: | 12.54050071 |
| mean anomaly at epoch: | 315.8211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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