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 68648U 26145.23825204 +.00000000 +00000-0 +43970-4 0 00006
2 68648 88.9877 323.3553 0010408 68.1945 292.0319 13.62731253 00
| Epoch (UTC): | 25 May 2026 05:43:04 |
| Eccentricity: | 0.0010408 |
| inclination: | 88.9877° |
| perigee height: | 1018 km |
| apogee height: | 1033 km |
| right ascension of ascending node: | 323.3553° |
| argument of perigee: | 68.1945° |
| revolutions per day: | 13.62731253 |
| mean anomaly at epoch: | 292.0319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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