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 00694U 26157.39790096 +.00000000 +00000-0 +25456-3 0 00001
2 00694 30.3534 59.7297 0546031 142.3465 221.6673 14.12493924 08
| Epoch (UTC): | 06 June 2026 09:32:58 |
| Eccentricity: | 0.0546031 |
| inclination: | 30.3534° |
| perigee height: | 456 km |
| apogee height: | 1246 km |
| right ascension of ascending node: | 59.7297° |
| argument of perigee: | 142.3465° |
| revolutions per day: | 14.12493924 |
| mean anomaly at epoch: | 221.6673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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