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 28898U 26121.37212205 +.00000000 +00000-0 +15078-3 0 00006
2 28898 98.3469 265.1416 0019477 125.1568 235.1462 14.64338683 06
| Epoch (UTC): | 01 May 2026 08:55:51 |
| Eccentricity: | 0.0019477 |
| inclination: | 98.3469° |
| perigee height: | 665 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 265.1416° |
| argument of perigee: | 125.1568° |
| revolutions per day: | 14.64338683 |
| mean anomaly at epoch: | 235.1462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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