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 65315U 26145.12134454 +.00000000 +00000-0 +19255-3 0 00000
2 65315 97.1970 221.6194 0002589 106.0556 254.0976 15.40806510 00
| Epoch (UTC): | 25 May 2026 02:54:44 |
| Eccentricity: | 0.0002589 |
| inclination: | 97.1970° |
| perigee height: | 442 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 221.6194° |
| argument of perigee: | 106.0556° |
| revolutions per day: | 15.40806510 |
| mean anomaly at epoch: | 254.0976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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