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 21263U 26067.91188183 +.00000000 +00000-0 +84714-4 0 00005
2 21263 98.6154 57.9252 0012983 325.6209 34.4130 14.26717322 09
| Epoch (UTC): | 08 March 2026 21:53:06 |
| Eccentricity: | 0.0012983 |
| inclination: | 98.6154° |
| perigee height: | 793 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 57.9252° |
| argument of perigee: | 325.6209° |
| revolutions per day: | 14.26717322 |
| mean anomaly at epoch: | 34.4130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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