▸Orbital parameters

Orbit class	SSO
Inclination	97.7588°
Eccentricity	0.0000754
Period	96.5 min
Apogee	592 km
Perigee	591 km
Mean motion	14.92043975 rev/day
RAAN	145.8418°
Arg of perigee	98.0642°
Mean anomaly	262.0662°
B*	1.7151e-4
Rev at epoch	1,466

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68486U 26067BY 26187.89373269 .00001685 00000-0 17151-3 0 9992

2 68486 97.7588 145.8418 0000754 98.0642 262.0662 14.92043975 14669

▸ source OMM (JSON)

{
  "OBJECT_NAME": "VINDLER 2.3",
  "OBJECT_ID": "2026-067BY",
  "EPOCH": "2026-07-06T21:26:58.504+00:00",
  "MEAN_MOTION": 14.92043975,
  "ECCENTRICITY": 0.0000754,
  "INCLINATION": 97.7588,
  "RA_OF_ASC_NODE": 145.8418,
  "ARG_OF_PERICENTER": 98.0642,
  "MEAN_ANOMALY": 262.0662,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68486,
  "REV_AT_EPOCH": 1466,
  "BSTAR": 0.00017151,
  "MEAN_MOTION_DOT": 0.00001685,
  "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.

▸Satellite metadata

Name	VINDLER 2.3
Operator	Sierra Nevada Corp.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	130HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68486

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.