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 26957U 01049A 25359.31863573 .13296088 27058-5 20609-3 0 9997
2 26957 97.8220 243.6447 0007632 25.7149 334.4532 16.48230161331525
| Epoch (UTC): | 25 December 2025 07:38:50 |
| Eccentricity: | 0.0007632 |
| inclination: | 97.8220° |
| perigee height: | 139 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 243.6447° |
| argument of perigee: | 25.7149° |
| revolutions per day: | 16.48230161 |
| mean anomaly at epoch: | 334.4532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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