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 26134.71596699 +.00000000 +00000-0 +00000-0 0 00005
2 38995 64.1054 0.0919 7340249 228.5613 40.2624 2.00654711 05
| Epoch (UTC): | 14 May 2026 17:10:59 |
| Eccentricity: | 0.7340249 |
| inclination: | 64.1054° |
| perigee height: | 684 km |
| apogee height: | 39664 km |
| right ascension of ascending node: | 0.0919° |
| argument of perigee: | 228.5613° |
| revolutions per day: | 2.00654711 |
| mean anomaly at epoch: | 40.2624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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