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 65178U 26145.22610823 +.00000000 +00000-0 +31420-3 0 00005
2 65178 97.4505 17.6674 0002590 86.0834 274.0689 15.05659970 08
| Epoch (UTC): | 25 May 2026 05:25:35 |
| Eccentricity: | 0.0002590 |
| inclination: | 97.4505° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6674° |
| argument of perigee: | 86.0834° |
| revolutions per day: | 15.05659970 |
| mean anomaly at epoch: | 274.0689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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