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 68470U 26145.37791182 +.00000000 +00000-0 +28973-3 0 00006
2 68470 97.4461 104.0334 0008235 136.0532 224.1358 15.17130097 00
| Epoch (UTC): | 25 May 2026 09:04:11 |
| Eccentricity: | 0.0008235 |
| inclination: | 97.4461° |
| perigee height: | 509 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 104.0334° |
| argument of perigee: | 136.0532° |
| revolutions per day: | 15.17130097 |
| mean anomaly at epoch: | 224.1358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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