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 68984U 26145.47778543 +.00000000 +00000-0 +13555-3 0 00003
2 68984 97.7365 43.3325 0003080 212.8900 147.2127 14.91099107 02
| Epoch (UTC): | 25 May 2026 11:28:00 |
| Eccentricity: | 0.0003080 |
| inclination: | 97.7365° |
| perigee height: | 592 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 43.3325° |
| argument of perigee: | 212.8900° |
| revolutions per day: | 14.91099107 |
| mean anomaly at epoch: | 147.2127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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