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 68408U 26145.60568394 +.00000000 +00000-0 +13166-3 0 00008
2 68408 97.4049 26.5917 0018283 83.9697 276.3621 15.18396749 05
| Epoch (UTC): | 25 May 2026 14:32:11 |
| Eccentricity: | 0.0018283 |
| inclination: | 97.4049° |
| perigee height: | 498 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 26.5917° |
| argument of perigee: | 83.9697° |
| revolutions per day: | 15.18396749 |
| mean anomaly at epoch: | 276.3621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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