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 65448U 26145.56139926 +.00000000 +00000-0 +20483-3 0 00009
2 65448 97.4517 359.7583 0002025 81.3354 278.8103 15.05657225 02
| Epoch (UTC): | 25 May 2026 13:28:24 |
| Eccentricity: | 0.0002025 |
| inclination: | 97.4517° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.7583° |
| argument of perigee: | 81.3354° |
| revolutions per day: | 15.05657225 |
| mean anomaly at epoch: | 278.8103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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