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 35681U 26115.48377127 +.00000000 +00000-0 +12777-3 0 00007
2 35681 97.7345 275.0143 0002076 47.2687 312.8697 14.75180899 09
| Epoch (UTC): | 25 April 2026 11:36:37 |
| Eccentricity: | 0.0002076 |
| inclination: | 97.7345° |
| perigee height: | 643 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 275.0143° |
| argument of perigee: | 47.2687° |
| revolutions per day: | 14.75180899 |
| mean anomaly at epoch: | 312.8697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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