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 65244U 26145.07879767 +.00000000 +00000-0 -34899-3 0 00000
2 65244 97.4518 187.9104 0001019 192.8280 167.2921 15.05628412 00
| Epoch (UTC): | 25 May 2026 01:53:28 |
| Eccentricity: | 0.0001019 |
| inclination: | 97.4518° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 187.9104° |
| argument of perigee: | 192.8280° |
| revolutions per day: | 15.05628412 |
| mean anomaly at epoch: | 167.2921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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