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 28414U 26070.84433546 +.00000000 +00000-0 +14762-3 0 00007
2 28414 97.6150 89.9722 0006589 106.6000 253.5951 15.05654931 06
| Epoch (UTC): | 11 March 2026 20:15:50 |
| Eccentricity: | 0.0006589 |
| inclination: | 97.6150° |
| perigee height: | 545 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 89.9722° |
| argument of perigee: | 106.6000° |
| revolutions per day: | 15.05654931 |
| mean anomaly at epoch: | 253.5951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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