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 16864U 26139.55142331 +.00000000 +00000-0 +58707-4 0 00004
2 16864 74.0275 181.0965 0032408 202.8213 157.1505 14.42310322 03
| Epoch (UTC): | 19 May 2026 13:14:02 |
| Eccentricity: | 0.0032408 |
| inclination: | 74.0275° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 181.0965° |
| argument of perigee: | 202.8213° |
| revolutions per day: | 14.42310322 |
| mean anomaly at epoch: | 157.1505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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