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 49173U 26145.12887132 +.00000000 +00000-0 -64784-5 0 00002
2 49173 70.0000 81.7193 0002408 266.0306 94.0577 14.98324417 04
| Epoch (UTC): | 25 May 2026 03:05:34 |
| Eccentricity: | 0.0002408 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.7193° |
| argument of perigee: | 266.0306° |
| revolutions per day: | 14.98324417 |
| mean anomaly at epoch: | 94.0577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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