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 68362U 26145.15610944 +.00000000 +00000-0 +37813-3 0 00001
2 68362 82.2972 38.4150 0002985 136.5478 223.6015 15.63466582 01
| Epoch (UTC): | 25 May 2026 03:44:47 |
| Eccentricity: | 0.0002985 |
| inclination: | 82.2972° |
| perigee height: | 376 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 38.4150° |
| argument of perigee: | 136.5478° |
| revolutions per day: | 15.63466582 |
| mean anomaly at epoch: | 223.6015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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