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 41179U 26145.17217580 +.00000000 +00000-0 +91890-4 0 00005
2 41179 47.0038 110.8128 0001316 82.6624 277.4411 14.58825699 09
| Epoch (UTC): | 25 May 2026 04:07:55 |
| Eccentricity: | 0.0001316 |
| inclination: | 47.0038° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 110.8128° |
| argument of perigee: | 82.6624° |
| revolutions per day: | 14.58825699 |
| mean anomaly at epoch: | 277.4411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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