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 65273U 26145.58748073 +.00000000 +00000-0 +14376-3 0 00000
2 65273 97.4484 198.1108 0001568 105.0800 255.0601 15.05654987 02
| Epoch (UTC): | 25 May 2026 14:05:58 |
| Eccentricity: | 0.0001568 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.1108° |
| argument of perigee: | 105.0800° |
| revolutions per day: | 15.05654987 |
| mean anomaly at epoch: | 255.0601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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