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 68154U 26145.04060042 +.00000000 +00000-0 +80604-4 0 00003
2 68154 97.2833 166.6239 0000152 184.7517 175.3724 15.33455834 02
| Epoch (UTC): | 25 May 2026 00:58:27 |
| Eccentricity: | 0.0000152 |
| inclination: | 97.2833° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.6239° |
| argument of perigee: | 184.7517° |
| revolutions per day: | 15.33455834 |
| mean anomaly at epoch: | 175.3724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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