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 38995U 26085.86424124 +.00000000 +00000-0 +00000-0 0 00009
2 38995 64.2728 7.0820 7330422 228.9159 40.0977 2.00563041 07
| Epoch (UTC): | 26 March 2026 20:44:30 |
| Eccentricity: | 0.7330422 |
| inclination: | 64.2728° |
| perigee height: | 712 km |
| apogee height: | 39652 km |
| right ascension of ascending node: | 7.0820° |
| argument of perigee: | 228.9159° |
| revolutions per day: | 2.00563041 |
| mean anomaly at epoch: | 40.0977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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