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 40012U 26038.26835671 +.00000000 +00000-0 +58307-3 0 00003
2 40012 97.7674 193.4783 0046538 135.8240 224.6708 14.87384634 00
| Epoch (UTC): | 07 February 2026 06:26:26 |
| Eccentricity: | 0.0046538 |
| inclination: | 97.7674° |
| perigee height: | 574 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 193.4783° |
| argument of perigee: | 135.8240° |
| revolutions per day: | 14.87384634 |
| mean anomaly at epoch: | 224.6708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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