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 26072.91389009 +.00000000 +00000-0 +33586-3 0 00001
2 39679 51.6070 316.6686 0097098 118.4391 242.6419 15.39329651 03
| Epoch (UTC): | 13 March 2026 21:56:00 |
| Eccentricity: | 0.0097098 |
| inclination: | 51.6070° |
| perigee height: | 382 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 316.6686° |
| argument of perigee: | 118.4391° |
| revolutions per day: | 15.39329651 |
| mean anomaly at epoch: | 242.6419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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