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 40071U 26032.48372726 +.00000000 +00000-0 +20916-3 0 00008
2 40071 98.3700 346.1442 0007352 6.4286 353.7022 14.89431255 02
| Epoch (UTC): | 01 February 2026 11:36:34 |
| Eccentricity: | 0.0007352 |
| inclination: | 98.3700° |
| perigee height: | 595 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 346.1442° |
| argument of perigee: | 6.4286° |
| revolutions per day: | 14.89431255 |
| mean anomaly at epoch: | 353.7022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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