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 13028U 26064.05460507 +.00000000 +00000-0 +11389-3 0 00007
2 13028 74.0388 281.6735 0020096 295.6513 64.2566 14.39871513 07
| Epoch (UTC): | 05 March 2026 01:18:37 |
| Eccentricity: | 0.0020096 |
| inclination: | 74.0388° |
| perigee height: | 745 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 281.6735° |
| argument of perigee: | 295.6513° |
| revolutions per day: | 14.39871513 |
| mean anomaly at epoch: | 64.2566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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