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 65132U 26145.43586794 +.00000000 +00000-0 +25942-3 0 00009
2 65132 51.8985 168.7022 0000400 67.5343 292.5662 14.79930091 08
| Epoch (UTC): | 25 May 2026 10:27:38 |
| Eccentricity: | 0.0000400 |
| inclination: | 51.8985° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 168.7022° |
| argument of perigee: | 67.5343° |
| revolutions per day: | 14.79930091 |
| mean anomaly at epoch: | 292.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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