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 68217U 26145.39635088 +.00000000 +00000-0 +40679-3 0 00006
2 68217 97.2864 20.8430 0001857 90.8118 269.3338 15.33450859 04
| Epoch (UTC): | 25 May 2026 09:30:44 |
| Eccentricity: | 0.0001857 |
| inclination: | 97.2864° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8430° |
| argument of perigee: | 90.8118° |
| revolutions per day: | 15.33450859 |
| mean anomaly at epoch: | 269.3338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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