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 03890U 26088.18475852 +.00000000 +00000-0 +24159-4 0 00002
2 03890 99.7178 331.9669 0039664 156.6618 322.5710 13.42667601 07
| Epoch (UTC): | 29 March 2026 04:26:03 |
| Eccentricity: | 0.0039664 |
| inclination: | 99.7178° |
| perigee height: | 1070 km |
| apogee height: | 1129 km |
| right ascension of ascending node: | 331.9669° |
| argument of perigee: | 156.6618° |
| revolutions per day: | 13.42667601 |
| mean anomaly at epoch: | 322.5710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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