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 05175U 26071.17130641 +.00000000 +00000-0 +74530-4 0 00003
2 05175 74.0458 95.4747 0030612 234.9836 124.8445 14.39476726 08
| Epoch (UTC): | 12 March 2026 04:06:40 |
| Eccentricity: | 0.0030612 |
| inclination: | 74.0458° |
| perigee height: | 738 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 95.4747° |
| argument of perigee: | 234.9836° |
| revolutions per day: | 14.39476726 |
| mean anomaly at epoch: | 124.8445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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