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 68496U 26145.63527649 +.00000000 +00000-0 +28237-3 0 00001
2 68496 97.7593 104.2678 0003030 55.8394 304.3111 14.92091237 04
| Epoch (UTC): | 25 May 2026 15:14:47 |
| Eccentricity: | 0.0003030 |
| inclination: | 97.7593° |
| perigee height: | 589 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 104.2678° |
| argument of perigee: | 55.8394° |
| revolutions per day: | 14.92091237 |
| mean anomaly at epoch: | 304.3111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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