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 07298U 26106.19243639 +.00000000 +00000-0 +00000-0 0 00001
2 07298 4.2961 249.1304 0016693 76.4713 135.4738 0.98614690 00
| Epoch (UTC): | 16 April 2026 04:37:06 |
| Eccentricity: | 0.0016693 |
| inclination: | 4.2961° |
| perigee height: | 36186 km |
| apogee height: | 36329 km |
| right ascension of ascending node: | 249.1304° |
| argument of perigee: | 76.4713° |
| revolutions per day: | 0.98614690 |
| mean anomaly at epoch: | 135.4738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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