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 64161U 26145.14031558 +.00000000 +00000-0 -17745-3 0 00004
2 64161 97.4532 196.5443 0002281 105.2352 254.9128 15.05631202 09
| Epoch (UTC): | 25 May 2026 03:22:03 |
| Eccentricity: | 0.0002281 |
| inclination: | 97.4532° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.5443° |
| argument of perigee: | 105.2352° |
| revolutions per day: | 15.05631202 |
| mean anomaly at epoch: | 254.9128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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