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 29268U 26150.53309220 +.00000000 +00000-0 +10731-3 0 00003
2 29268 97.8303 335.8346 0015537 126.0793 308.5014 14.64647928 02
| Epoch (UTC): | 30 May 2026 12:47:39 |
| Eccentricity: | 0.0015537 |
| inclination: | 97.8303° |
| perigee height: | 667 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 335.8346° |
| argument of perigee: | 126.0793° |
| revolutions per day: | 14.64647928 |
| mean anomaly at epoch: | 308.5014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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