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 03029U 26032.14975390 +.00000000 +00000-0 +00000-0 0 00008
2 03029 2.8279 80.0025 0014318 30.3524 329.6216 1.00271724 06
| Epoch (UTC): | 01 February 2026 03:35:38 |
| Eccentricity: | 0.0014318 |
| inclination: | 2.8279° |
| perigee height: | 35726 km |
| apogee height: | 35847 km |
| right ascension of ascending node: | 80.0025° |
| argument of perigee: | 30.3524° |
| revolutions per day: | 1.00271724 |
| mean anomaly at epoch: | 329.6216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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