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 38753U 26052.83006360 +.00000000 +00000-0 +63262-3 0 00002
2 38753 10.1185 217.0821 6392754 358.3947 0.1727 3.47611967 01
| Epoch (UTC): | 21 February 2026 19:55:17 |
| Eccentricity: | 0.6392754 |
| inclination: | 10.1185° |
| perigee height: | 262 km |
| apogee height: | 23798 km |
| right ascension of ascending node: | 217.0821° |
| argument of perigee: | 358.3947° |
| revolutions per day: | 3.47611967 |
| mean anomaly at epoch: | 0.1727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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