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 49402U 26145.06993241 +.00000000 +00000-0 +25441-3 0 00003
2 49402 97.3207 187.6803 0011903 291.3952 68.6016 15.26464520 09
| Epoch (UTC): | 25 May 2026 01:40:42 |
| Eccentricity: | 0.0011903 |
| inclination: | 97.3207° |
| perigee height: | 478 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 187.6803° |
| argument of perigee: | 291.3952° |
| revolutions per day: | 15.26464520 |
| mean anomaly at epoch: | 68.6016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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