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 63304U 26145.58390851 +.00000000 +00000-0 +10373-3 0 00003
2 63304 97.9093 270.2877 0005743 25.4374 334.7115 14.72273675 00
| Epoch (UTC): | 25 May 2026 14:00:49 |
| Eccentricity: | 0.0005743 |
| inclination: | 97.9093° |
| perigee height: | 650 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 270.2877° |
| argument of perigee: | 25.4374° |
| revolutions per day: | 14.72273675 |
| mean anomaly at epoch: | 334.7115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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