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 68147U 26145.02158563 +.00000000 +00000-0 +69990-3 0 00003
2 68147 97.2836 166.6559 0001750 91.9965 268.1478 15.33451452 02
| Epoch (UTC): | 25 May 2026 00:31:04 |
| Eccentricity: | 0.0001750 |
| inclination: | 97.2836° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 166.6559° |
| argument of perigee: | 91.9965° |
| revolutions per day: | 15.33451452 |
| mean anomaly at epoch: | 268.1478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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