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 04168U 26087.88999002 +.00000000 +00000-0 +69505-4 0 00009
2 04168 70.0123 269.5403 0022132 235.0573 124.8454 13.96001394 02
| Epoch (UTC): | 28 March 2026 21:21:35 |
| Eccentricity: | 0.0022132 |
| inclination: | 70.0123° |
| perigee height: | 892 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 269.5403° |
| argument of perigee: | 235.0573° |
| revolutions per day: | 13.96001394 |
| mean anomaly at epoch: | 124.8454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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