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 26150.51403064 +.00000000 +00000-0 +51035-3 0 00006
2 28414 97.6059 168.6087 0004476 176.2102 183.9159 15.06180880 06
| Epoch (UTC): | 30 May 2026 12:20:12 |
| Eccentricity: | 0.0004476 |
| inclination: | 97.6059° |
| perigee height: | 545 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 168.6087° |
| argument of perigee: | 176.2102° |
| revolutions per day: | 15.06180880 |
| mean anomaly at epoch: | 183.9159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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