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 37793U 26133.26587323 +.00000000 +00000-0 +56100-4 0 00009
2 37793 98.2385 43.0503 0042676 195.9977 281.9310 14.76866079 01
| Epoch (UTC): | 13 May 2026 06:22:51 |
| Eccentricity: | 0.0042676 |
| inclination: | 98.2385° |
| perigee height: | 609 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 43.0503° |
| argument of perigee: | 195.9977° |
| revolutions per day: | 14.76866079 |
| mean anomaly at epoch: | 281.9310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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