▸Orbital parameters

Orbit class	SSO
Inclination	97.4705°
Eccentricity	0.0005140
Period	97.2 min
Apogee	628 km
Perigee	621 km
Mean motion	14.81423907 rev/day
RAAN	249.0087°
Arg of perigee	254.4446°
Mean anomaly	105.6200°
B*	1.6870e-4
Rev at epoch	22,332

▸Two-line element set (TLE)

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

1 52771U 22057AR 26187.98092104 .00001273 00000-0 16870-3 0 9993

2 52771 97.4705 249.0087 0005140 254.4446 105.6200 14.81423907223320

▸ source OMM (JSON)

{
  "OBJECT_NAME": "OMNI-L2",
  "OBJECT_ID": "2022-057AR",
  "EPOCH": "2026-07-06T23:32:31.578+00:00",
  "MEAN_MOTION": 14.81423907,
  "ECCENTRICITY": 0.000514,
  "INCLINATION": 97.4705,
  "RA_OF_ASC_NODE": 249.0087,
  "ARG_OF_PERICENTER": 254.4446,
  "MEAN_ANOMALY": 105.62,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52771,
  "REV_AT_EPOCH": 22332,
  "BSTAR": 0.0001687,
  "MEAN_MOTION_DOT": 0.00001273,
  "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	OMNI-L2
Operator	OmniSpace LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	May 25, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	20HIGHvia 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/52771

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