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 65181U 26145.62209014 +.00000000 +00000-0 +19315-3 0 00008
2 65181 97.4476 18.0556 0002470 88.1158 272.0352 15.05657190 09
| Epoch (UTC): | 25 May 2026 14:55:48 |
| Eccentricity: | 0.0002470 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0556° |
| argument of perigee: | 88.1158° |
| revolutions per day: | 15.05657190 |
| mean anomaly at epoch: | 272.0352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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