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 13002U 26065.32501905 +.00000000 +00000-0 -33303-3 0 00009
2 13002 82.9667 356.4052 0050884 263.7051 213.4714 12.13844963 03
| Epoch (UTC): | 06 March 2026 07:48:01 |
| Eccentricity: | 0.0050884 |
| inclination: | 82.9667° |
| perigee height: | 1579 km |
| apogee height: | 1660 km |
| right ascension of ascending node: | 356.4052° |
| argument of perigee: | 263.7051° |
| revolutions per day: | 12.13844963 |
| mean anomaly at epoch: | 213.4714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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