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 52898U 26121.92360964 +.00000000 +00000-0 +21109-3 0 00002
2 52898 98.2138 266.3176 0008225 161.5280 198.6222 14.63611756 06
| Epoch (UTC): | 01 May 2026 22:09:59 |
| Eccentricity: | 0.0008225 |
| inclination: | 98.2138° |
| perigee height: | 676 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 266.3176° |
| argument of perigee: | 161.5280° |
| revolutions per day: | 14.63611756 |
| mean anomaly at epoch: | 198.6222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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