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 39679U 26067.91474416 +.00000000 +00000-0 +42013-3 0 00007
2 39679 51.6074 341.0593 0097618 100.2042 260.9968 15.39151766 08
| Epoch (UTC): | 08 March 2026 21:57:13 |
| Eccentricity: | 0.0097618 |
| inclination: | 51.6074° |
| perigee height: | 382 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 341.0593° |
| argument of perigee: | 100.2042° |
| revolutions per day: | 15.39151766 |
| mean anomaly at epoch: | 260.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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