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 35935U 26038.19015382 +.00000000 +00000-0 +30248-3 0 00006
2 35935 98.4146 303.0142 0006313 286.2777 73.7728 14.60199186 03
| Epoch (UTC): | 07 February 2026 04:33:49 |
| Eccentricity: | 0.0006313 |
| inclination: | 98.4146° |
| perigee height: | 688 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 303.0142° |
| argument of perigee: | 286.2777° |
| revolutions per day: | 14.60199186 |
| mean anomaly at epoch: | 73.7728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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