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 data is extracted from the following two-line orbital elements,
1 26958U 01049B 25322.51542584 .00003230 00000-0 21643-3 0 9999
2 26958 97.9586 318.8934 0058040 114.0570 246.6744 15.06270263311894
| Epoch (UTC): | 18 November 2025 12:22:12 |
| Eccentricity: | 0.0058040 |
| inclination: | 97.9586° |
| perigee height: | 507 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 318.8934° |
| argument of perigee: | 114.0570° |
| revolutions per day: | 15.06270263 |
| mean anomaly at epoch: | 246.6744° |
| orbit number at epoch: | 31189 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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