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 20103U 26106.20709317 +.00000000 +00000-0 +50744-4 0 00007
2 20103 82.9635 347.2601 0036098 281.4274 195.8415 13.74846666 02
| Epoch (UTC): | 16 April 2026 04:58:12 |
| Eccentricity: | 0.0036098 |
| inclination: | 82.9635° |
| perigee height: | 956 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 347.2601° |
| argument of perigee: | 281.4274° |
| revolutions per day: | 13.74846666 |
| mean anomaly at epoch: | 195.8415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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