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 37775U 26145.58754177 +.00000000 +00000-0 +00000-0 0 00004
2 37775 0.0895 43.2971 0005902 35.6360 34.9494 1.00271908 09
| Epoch (UTC): | 25 May 2026 14:06:03 |
| Eccentricity: | 0.0005902 |
| inclination: | 0.0895° |
| perigee height: | 35762 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 43.2971° |
| argument of perigee: | 35.6360° |
| revolutions per day: | 1.00271908 |
| mean anomaly at epoch: | 34.9494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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