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 49161U 26145.25424619 +.00000000 +00000-0 +24936-3 0 00002
2 49161 69.9990 101.3884 0003859 256.8742 103.1987 14.98360086 03
| Epoch (UTC): | 25 May 2026 06:06:06 |
| Eccentricity: | 0.0003859 |
| inclination: | 69.9990° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 101.3884° |
| argument of perigee: | 256.8742° |
| revolutions per day: | 14.98360086 |
| mean anomaly at epoch: | 103.1987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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