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 26032.00794963 +.00000000 +00000-0 +00000-0 0 00008
2 38995 64.3299 14.6401 7316160 229.3097 40.0350 2.00518700 06
| Epoch (UTC): | 01 February 2026 00:11:26 |
| Eccentricity: | 0.7316160 |
| inclination: | 64.3299° |
| perigee height: | 751 km |
| apogee height: | 39621 km |
| right ascension of ascending node: | 14.6401° |
| argument of perigee: | 229.3097° |
| revolutions per day: | 2.00518700 |
| mean anomaly at epoch: | 40.0350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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