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 26103.81232649 +.00000000 +00000-0 +00000-0 0 00004
2 38995 64.1761 4.5596 7333552 228.7702 40.1584 2.00593975 08
| Epoch (UTC): | 13 April 2026 19:29:45 |
| Eccentricity: | 0.7333552 |
| inclination: | 64.1761° |
| perigee height: | 703 km |
| apogee height: | 39656 km |
| right ascension of ascending node: | 4.5596° |
| argument of perigee: | 228.7702° |
| revolutions per day: | 2.00593975 |
| mean anomaly at epoch: | 40.1584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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