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 29479U 26032.32097059 +.00000000 +00000-0 +14648-3 0 00008
2 29479 98.0635 50.4358 0017532 3.6828 356.4503 14.68407924 05
| Epoch (UTC): | 01 February 2026 07:42:11 |
| Eccentricity: | 0.0017532 |
| inclination: | 98.0635° |
| perigee height: | 654 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 50.4358° |
| argument of perigee: | 3.6828° |
| revolutions per day: | 14.68407924 |
| mean anomaly at epoch: | 356.4503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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