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 68228U 26145.23593255 +.00000000 +00000-0 +58274-3 0 00000
2 68228 97.2864 20.7560 0001876 94.2269 265.9188 15.33451246 01
| Epoch (UTC): | 25 May 2026 05:39:44 |
| Eccentricity: | 0.0001876 |
| inclination: | 97.2864° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.7560° |
| argument of perigee: | 94.2269° |
| revolutions per day: | 15.33451246 |
| mean anomaly at epoch: | 265.9188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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