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 52900U 26067.35786817 +.00000000 +00000-0 +23110-3 0 00005
2 52900 98.2080 210.4454 0007239 350.7029 9.4037 14.61709068 07
| Epoch (UTC): | 08 March 2026 08:35:19 |
| Eccentricity: | 0.0007239 |
| inclination: | 98.2080° |
| perigee height: | 683 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 210.4454° |
| argument of perigee: | 350.7029° |
| revolutions per day: | 14.61709068 |
| mean anomaly at epoch: | 9.4037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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