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 68158U 26145.29619920 +.00000000 +00000-0 +34696-3 0 00008
2 68158 97.2846 166.8927 0001192 101.8337 258.3040 15.33449620 00
| Epoch (UTC): | 25 May 2026 07:06:31 |
| Eccentricity: | 0.0001192 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.8927° |
| argument of perigee: | 101.8337° |
| revolutions per day: | 15.33449620 |
| mean anomaly at epoch: | 258.3040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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