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 35933U 26038.17522441 +.00000000 +00000-0 +32106-3 0 00006
2 35933 98.4057 303.6742 0004052 274.8438 85.2300 14.61458243 06
| Epoch (UTC): | 07 February 2026 04:12:19 |
| Eccentricity: | 0.0004052 |
| inclination: | 98.4057° |
| perigee height: | 686 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 303.6742° |
| argument of perigee: | 274.8438° |
| revolutions per day: | 14.61458243 |
| mean anomaly at epoch: | 85.2300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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