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 42285U 26067.30977384 +.00000000 +00000-0 +23073-2 0 00003
2 42285 98.9048 97.6141 0028995 320.5998 39.3072 14.26598707 01
| Epoch (UTC): | 08 March 2026 07:26:04 |
| Eccentricity: | 0.0028995 |
| inclination: | 98.9048° |
| perigee height: | 782 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 97.6141° |
| argument of perigee: | 320.5998° |
| revolutions per day: | 14.26598707 |
| mean anomaly at epoch: | 39.3072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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