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 28894U 26154.32033494 +.00000000 +00000-0 +11613-3 0 00005
2 28894 98.3061 294.1550 0015089 326.7589 33.2665 14.65360624 01
| Epoch (UTC): | 03 June 2026 07:41:16 |
| Eccentricity: | 0.0015089 |
| inclination: | 98.3061° |
| perigee height: | 665 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 294.1550° |
| argument of perigee: | 326.7589° |
| revolutions per day: | 14.65360624 |
| mean anomaly at epoch: | 33.2665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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