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 68394U 26145.64842338 +.00000000 +00000-0 +59938-3 0 00006
2 68394 97.2860 288.2725 0000879 100.5210 259.6132 15.33456010 07
| Epoch (UTC): | 25 May 2026 15:33:43 |
| Eccentricity: | 0.0000879 |
| inclination: | 97.2860° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 288.2725° |
| argument of perigee: | 100.5210° |
| revolutions per day: | 15.33456010 |
| mean anomaly at epoch: | 259.6132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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