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 68030U 26145.35925366 +.00000000 +00000-0 +68300-3 0 00007
2 68030 97.2847 94.3864 0002355 91.4451 268.7061 15.33448681 02
| Epoch (UTC): | 25 May 2026 08:37:19 |
| Eccentricity: | 0.0002355 |
| inclination: | 97.2847° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3864° |
| argument of perigee: | 91.4451° |
| revolutions per day: | 15.33448681 |
| mean anomaly at epoch: | 268.7061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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