VINDLER 2.1 is a payload in SSO orbit, operated by Sierra Nevada Corp., launched 2026.
| Orbit class | SSO |
| Inclination | 97.7582° |
| Eccentricity | 0.0001657 |
| Period | 96.5 min |
| Apogee | 593 km |
| Perigee | 590 km |
| Mean motion | 14.92047018 rev/day |
| RAAN | 145.8358° |
| Arg of perigee | 44.7890° |
| Mean anomaly | 315.3462° |
| B* | 1.7381e-4 |
| Rev at epoch | 1,466 |
1 68488U 26067CA 26187.89401494 .00001708 00000-0 17381-3 0 99972 68488 97.7582 145.8358 0001657 44.7890 315.3462 14.92047018 14666{
"OBJECT_NAME": "VINDLER 2.1",
"OBJECT_ID": "2026-067CA",
"EPOCH": "2026-07-06T21:27:22.891+00:00",
"MEAN_MOTION": 14.92047018,
"ECCENTRICITY": 0.0001657,
"INCLINATION": 97.7582,
"RA_OF_ASC_NODE": 145.8358,
"ARG_OF_PERICENTER": 44.789,
"MEAN_ANOMALY": 315.3462,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68488,
"REV_AT_EPOCH": 1466,
"BSTAR": 0.00017381,
"MEAN_MOTION_DOT": 0.00001708,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | VINDLER 2.1 |
| Operator | |
| Country | United States |
| Launch date | |
| Launch mass (kg) |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |