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 68198U 26145.64846718 +.00000000 +00000-0 +32006-3 0 00001
2 68198 97.5330 220.7715 0013874 32.5917 327.6166 15.10633610 02
| Epoch (UTC): | 25 May 2026 15:33:47 |
| Eccentricity: | 0.0013874 |
| inclination: | 97.5330° |
| perigee height: | 525 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 220.7715° |
| argument of perigee: | 32.5917° |
| revolutions per day: | 15.10633610 |
| mean anomaly at epoch: | 327.6166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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