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 68378U 26145.43429954 +.00000000 +00000-0 +73599-4 0 00000
2 68378 97.4384 153.0680 0001565 114.8596 245.2802 15.19722869 06
| Epoch (UTC): | 25 May 2026 10:25:23 |
| Eccentricity: | 0.0001565 |
| inclination: | 97.4384° |
| perigee height: | 506 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 153.0680° |
| argument of perigee: | 114.8596° |
| revolutions per day: | 15.19722869 |
| mean anomaly at epoch: | 245.2802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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