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 35683U 26077.85654887 +.00000000 +00000-0 +85578-4 0 00008
2 35683 97.8663 215.1159 0001249 96.9595 263.1757 14.75871317 04
| Epoch (UTC): | 18 March 2026 20:33:25 |
| Eccentricity: | 0.0001249 |
| inclination: | 97.8663° |
| perigee height: | 642 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 215.1159° |
| argument of perigee: | 96.9595° |
| revolutions per day: | 14.75871317 |
| mean anomaly at epoch: | 263.1757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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