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 68893U 26142.50683609 +.00000000 +00000-0 +00000-0 0 00009
2 68893 2.3429 280.4148 1281814 181.0731 252.6119 1.26078027 08
| Epoch (UTC): | 22 May 2026 12:09:50 |
| Eccentricity: | 0.1281814 |
| inclination: | 2.3429° |
| perigee height: | 25177 km |
| apogee height: | 34456 km |
| right ascension of ascending node: | 280.4148° |
| argument of perigee: | 181.0731° |
| revolutions per day: | 1.26078027 |
| mean anomaly at epoch: | 252.6119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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