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 38991U 26145.49763163 +.00000000 +00000-0 +00000-0 0 00000
2 38991 0.0264 276.9028 0002687 166.6933 263.6406 1.00271479 03
| Epoch (UTC): | 25 May 2026 11:56:35 |
| Eccentricity: | 0.0002687 |
| inclination: | 0.0264° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 276.9028° |
| argument of perigee: | 166.6933° |
| revolutions per day: | 1.00271479 |
| mean anomaly at epoch: | 263.6406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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