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 40025U 26066.46658970 +.00000000 +00000-0 +76648-3 0 00003
2 40025 98.1011 70.5993 0008061 202.2210 157.8673 15.16461889 06
| Epoch (UTC): | 07 March 2026 11:11:53 |
| Eccentricity: | 0.0008061 |
| inclination: | 98.1011° |
| perigee height: | 511 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 70.5993° |
| argument of perigee: | 202.2210° |
| revolutions per day: | 15.16461889 |
| mean anomaly at epoch: | 157.8673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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